Minimization of Ground Vibration Test Configurations for F-16 Aircraft by Subtractive Modification

Table 1

Modal parameters calculated using the equivalent FE model.

Mode number	Frequency (Hz)
1	4.85
2	4.95
3	5.23
4	5.79
5	7.01
6	12.18
7	15.33
8	15.39
9	15.40
10	15.65
11	16.91
12	17.46
13	24.21
14	24.33